PA-32 Cherokee Six vs SR-71 Blackbird
Overview
The PA-32 Cherokee Six and the SR-71 Blackbird are both Military Special Mission Aircraft, manufactured by Piper and Lockheed respectively.
The SR-71 Blackbird reaches 3,541 km/h β 16:1 the PA-32 Cherokee Six's 228 km/h. The PA-32 Cherokee Six has an operational range of 1,361 km vs 5,230 km for the SR-71 Blackbird. The SR-71 Blackbird operates at altitudes up to 25,908 m compared to 4,359 m for the PA-32 Cherokee Six. At 78,018 kg MTOW, the SR-71 Blackbird is 80:1 the PA-32 Cherokee Six's 975 kg.
The PA-32 Cherokee Six has been produced in 7,842 units vs 32 for the SR-71 Blackbird. The PA-32 Cherokee Six first flew 4 years before the SR-71 Blackbird (1960 vs 1964).
| American light, single-engined aircraft, dominant during the late 20th century, widely used for personal, commercial air taxi services. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Piper |
| First flight | 14 January 1960 |
| Year introduced | 1965 |
| Number produced | 7842 units |
| Average unit price | -- |
| American strategic reconnaissance aircraft, operational from 1966-1998, unmatched speed and altitude records, infamous for Cold War and NASA missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Lockheed |
| First flight | 22 December 1964 |
| Year introduced | 1966 |
| Number produced | 32 units |
| Average unit price | $185 million |
| Wing area | 15.0 mΒ² β |
| Wingspan | 9.0 m β |
| Height | 2.2 m β |
| Length | 7.1 m β |
| Maximum speed | 228 km/h β |
| Operational range | 1,361 km β |
| Service ceiling | 4,359 m β |
| Max. takeoff weight | 975 kg β |
| Empty weight | 545 kg β |
| Total thrust | 1 x 112 kW β |
| Wing area | 167.0 mΒ² β |
| Wingspan | 17.0 m β |
| Height | 5.7 m β |
| Length | 32.8 m β |
| Maximum speed | 3541 km/h β |
| Operational range | 5,230 km β |
| Service ceiling | 25,908 m β |
| Max. takeoff weight | 78,018 kg β |
| Empty weight | 30,617 kg β |
| Total thrust | 2 x 5,670 kgf β |
Performance Radar Chart
Detailed Comparison
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